Pilots should not exchange seats during flight if only two pilots are aboard the airplane (T/F)
True
Verbal coordination between the pilot flying
... [Show More] the aircraft and the applicable crew member will be required when
Any of the above
Normal hydraulic pressure range is ____ to ___ psi
2400 - 3050 psi
Maximum EGT during engine start is ____ degrees C
725
EGT between _____ is limited to 5 min duration.
EGT between ____ - retard the throttle to bring EGT to within limits.
Operation is allowed until the next landing, if the EGT exceeds ______ - shut down the engine using ENGINE FIRE FAILURE DURING FLIGHT checklist
870 - 905 C
906 - 930 C
930 C
Normal oil pressure limits are ____ psi. Oil pressure fluctuations of not more than ___ psi total are allowed. As long as they remain within normal limits
11 - 92
10
Moderate to severe airplane buffeting can occur with simultaneous use of speed brakes and flaps. This buffeting can result in damage or loss of airplane surfaces
True
Because of possible damage due to sonic airflow at certain angles of attack, do not extend flaps above ___ feet pressure altitude
20,000
The t/o and emergency procedures portion will be reviewed just prior to
Engien start OR takeoff
B or C answer
Based on _____, the aircraft commander may elect single pilot preflight ops where one pilot proceeds to the aircraft with the boom op to perform the exterior safety check and begin the interior preflight checks, while the other pilot accomplishes additional duties (wx brief, etc)
A or B
Operational need OR mission requirements.
All crewmembers will inform the pilot when checking off and/or on interphone and will be on interphone during
All of the above
Because of the magnitude of interrelated aerodynamic affects, flying to airplanes in close vertical proximity is
not safe
Speed brakes are NOT used during approach and landing flare
True
All snow and ice accumulations of any significant degree must be removed from the airplane surfaces prior to takeoff
True
If the _____ is not down and in the detent, ensure that the _____ is installed. Notify the AC and mx personell immediately. No further preflight actions will be accomplished until mx personell correct the situation and confirm that the aircraft is preflight config
Landing gear level
nose gear ground downlock and release handle
The pilot will ensure that no personnel are standing near the _________________ when pressurizing the left hydraulic system.
wheel well doors
The copilot ANN DIM switch on the co overhead light panel must be out of the DIM (full ccw) position for the____ to operate. Ensure it is out of full dim prior to closing the crew door. Once closed, the switch can be adjusted
FDR
Possible causes of a ____ are engaging the pilot's interphone (on the yoke or the tiller) pressing the pilots FD ANN TEST button, a cold hydraulic system, the low-flow capability of the aux hydraulic pump, and/or the use of other hydraulically actuated systems during the EFAS test, in this case, the EFAS self-test is ______ indicating a system failure
Failed EFAS test
incorrectly
Speed brake warning horn sounds when the level is pulled back more than ___ degrees out of the full forward position
2
Proper adjustment of the ____ is especially critical for takeoff, approach, and landing where full deflection of control surfaces may be required for safe operation of the airplane. To prevent inadvertent movement of the seat, ensure that the ____ is in the down and latched position
Seat and rudder pedals
seat horizontal adjustment lever
If an APU with an operable generator is not available, and external power is not used, the start can be made on battery power only. During this procedure, all engine ____ gages are inop until a generator is on the line and 28V AC power is available.
Oil pressure and fuel flow
Copilot checks for initial fuel flow peak of ____ pph (before ignition) and approximately ___ pph after ignition. If fuel flow exceeds ____ pph before lightoff, a hot start can occur
300-680
900
680
For temps ____, failure to set the engine start switch to IGNITION may result in engine flameout when the throttles are retarded during taxi ops
At and below 0C (32F)
Items 18 - 29 of the starting engines and before taxi checklist may be accomplished while waiting for the ground crew report
True
Min taxi width is ___ feet
74 feet
Do not taxi, or tow an aircraft within ____ of obstructions without wing walkers monitoring
clearance between aircraft and obstruction, and do not taxi closer than _____ to any obstacles
25
10
When taxi clrc is doubtful, use ___ wing walkers
one or more
Make every effort to min the potential for engine FOD. crews should
All of the above
What is the min taxi space during formation
safe interval
during night taxi operations, marshallers will have ____ in each hand
An illuminated wand
AF pilots may passively participate in LAHSO (land or t/o when another aircraft has been given LAHSO clrc). PIC is the final authority whether to t/o, land, continue a touch and go when a merging aircraft recieved a LAHSO clrc
True
When must aircraft anti-collision lights be displayed
from just prior to engine start until engine shutdown
you are approaching another aircraft on the ground head on, what should you do
alter the course to their right to remain well clear, or stop
When taxi clrc is doubtful and wing walkers are not available
Deplane one or more crew members to maintain obstruction clrc and provide marshaling using AFI 11-218 signals
In those situations where runway/taxi conditions or performance considerations are such that safety could be compromosed
a static takeoff should be made
For a t/o, approach, or lndg with fuel in any main tank below _____ pounds, open all tank to engine manifold valves. Open the line valve for t/o when gross weight is greater than _____ pounds. Ensure the line valve is closed for all takeoffs when gross weight is at or below _____ pounds
10,500
200,000
200,000
Exercise caution during throttle application to prevent asymmetrical thrust. Engine thrust should be stabilized at a minimum of ___ prior to advancing throttles to takeoff thrust setting
40% N1
Uncommanded stab trim input is a safety of flight issue. Terminate the mission (and in flight, land as soon as practicable) any time uncommanded stab trim is encountered
True
If any engine does not reach the charted N1 setting ______ the engine is not providing the required rated thrust, and the T/o should be aborted
Between 40 and 80 knots
Illumination of amber EGT caution light near or after S1 indicates the EGT may be approaching t/o limit. Indication is for crew awareness and does not indicate an engine op limit being exceedd. continue normal op and monitor EGT to prevent exceeding the takeoff limit
True
When ___ throttle is advanced near open, the warning horn sounds if the speed brakes lever is more than 2 degrees out of the full forward position. If the flap lever is at or near the 0 40 or 50 degree detent, or the leading edge flaps are not full extended
No 3
The sudden reversal of rudder direction at high rudder deflections, due to improper rudder application or abrupt release, can result in _____.
over stressing the vertical fin
If stab trim has moved from setting selected during the taxi checklist.______
abort the mission
When experiencing a loss shear on t/o, anticipate a loss in indicated airspeed and altitude. This situation is potentially dangerous if the airplane is close to the ground. If this loss is expected to be ____ kts or more, the t/o shall be delayed, if possible, until more favourable conditions exist
15
When the airplane is definitely airborne and a positve rate of climb is estblshed, retract the landing gear
True
Follow -1 procedures for the climb mode selected until reaching ____ or obstacle clearance height, whichever is higher
2000 ft above the runway
Leave ignition on if engine anti-ice is on. If not required, turn starter switches off _____
5 min after establisehd at cruise altitude [Show Less]